发明名称 |
Simplified anti-vibration suspension for helicopter rotor |
摘要 |
The anti-vibration suspension comprises three inclined bars (8) each articulated (9,11) on the structure (1) and the on the transmission box (2) by a rigid lever (12). The lever which supports a swinging mass (13) is pivoted on the transmission box. For each inclined bar a traction bar (16) is also articulated (17,18) on the structure and the transmission box. The corresponding lever is articulated on the box by pivoting on the upper end part of the corresponding traction bar.
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申请公布号 |
FR2777860(A1) |
申请公布日期 |
1999.10.29 |
申请号 |
FR19980005093 |
申请日期 |
1998.04.23 |
申请人 |
EUROCOPTER FRANCE |
发明人 |
CERTAIN NICOLAS PIERRE GEORGES |
分类号 |
B64C27/00;(IPC1-7):B64C27/00;F16F7/10;F16F15/04;F16F15/28 |
主分类号 |
B64C27/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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